Using shock control bumps to improve engine intake performance and operability

John, A., Bower, J., Qin, N. orcid.org/0000-0002-6437-9027 et al. (2 more authors) (2020) Using shock control bumps to improve engine intake performance and operability. The Aeronautical Journal, 124 (1282). pp. 1913-1944. ISSN 0001-9240

Abstract

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Authors/Creators:
Copyright, Publisher and Additional Information: © The Author(s), 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society. This is an author produced version of a paper subsequently published in Aeronautical Journal. Article available under the terms of the CC-BY-NC-ND license (https://creativecommons.org/licenses/by-nc-nd/4.0/).
Keywords: Intake; Aerodynamics; Shock Control; Separation; Optimisation
Dates:
  • Published (online): 23 November 2020
  • Published: December 2020
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Funding Information:
FunderGrant number
ROLLS-ROYCE PLC (UK)5002531676
Depositing User: Symplectic Sheffield
Date Deposited: 28 Jan 2021 11:54
Last Modified: 23 May 2021 00:38
Status: Published
Publisher: Cambridge University Press (CUP)
Refereed: Yes
Identification Number: https://doi.org/10.1017/aer.2020.87
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